Podélná a stranová dynamická stabilita letounu

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F04%3APU48266" target="_blank" >RIV/00216305:26210/04:PU48266 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

čeština

Název v původním jazyce

Podélná a stranová dynamická stabilita letounu

Popis výsledku v původním jazyce

The dynamic stability control presents one of the important parts of flight characteristics analysis of design atmospheric aircraft. The dynamic stability calculations, following aircraft from its primary design, have a great influence on the final aircraft appearance. The suitability of proposed aircraft design and possible modifications will appear just during the flight tests. The results of flight tests are used for the verification of applied theory and for the verification of designed aircraft stability and control as well. This paper presents the issue of flight measurement and theory calculations of dynamic stability. It is dealing in detail with comparison of performed flight measurements and computations. The aircraft, mainly supporting thisresearch, is the two-seat all-metal motor glider L-13 SE Vivat

Název v anglickém jazyce

Longitudinal and Lateral Dynamic Stability

Popis výsledku anglicky

The dynamic stability control presents one of the important parts of flight characteristics analysis of design atmospheric aircraft. The dynamic stability calculations, following aircraft from its primary design, have a great influence on the final aircraft appearance. The suitability of proposed aircraft design and possible modifications will appear just during the flight tests. The results of flight tests are used for the verification of applied theory and for the verification of designed aircraft stability and control as well. This paper presents the issue of flight measurement and theory calculations of dynamic stability. It is dealing in detail with comparison of performed flight measurements and computations. The aircraft, mainly supporting thisresearch, is the two-seat all-metal motor glider L-13 SE Vivat

Druh

A - Audiovizuální tvorba

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

<a href="/cs/project/LN00B051" target="_blank" >LN00B051: Centrum leteckého a kosmického výzkumu (CLKV)</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2004

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

ISBN

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Místo vydání

Praha

Název nakladatele resp. objednatele

Výzkumný a zkušební letecký ústav

Verze

neuvedeno

Identifikační číslo nosiče

neuvedeno